Aerodynamic layout structure of foldable full-motion double wings

The invention belongs to the technical field of aircraft design, and discloses a foldable all-moving double-wing pneumatic layout structure, two front guide rails and two rear guide rails are symmetrically arranged on two sides of the middle section of an unmanned aerial vehicle body, two front all-moving wings are connected to servo mechanisms in the two front guide rails respectively, and two rear all-moving wings are connected to servo mechanisms in the two rear guide rails respectively; the two rear all-moving wings are respectively connected to the servo mechanisms in the two rear guide rails; and the servo mechanism moves and rotates in the guide rail. The controllable pneumatic surfaces are arranged in a concentrated mode, various control modes such as translation, differential motion, follow-up and rotation around a force bearing shaft can be adopted, the flight control range of the unmanned aerial vehicle is greatly widened, enough operation space is reserved for high-maneuverability actions of the u